In the field of antenna reflectors with a deformable reflecting surface, an actuation system, with which such a reflector may be equipped wherein the reflector includes a chassis, a flexible membrane fixed to the chassis, comprises: a support fixed to the chassis, a set of deformation devices, each deformation device including a pusher element adapted to be driven in translation relative to the support along an axis, the pusher element including a part adapted to come into contact with the flexible membrane at a point to deform it, an actuation device adapted to drive the pusher element of one of the deformation devices in translation at the same time, and a selector device adapted to move the actuation device toward each of the deformation devices.
|
9. A reflector, comprising:
a chassis;
a flexible membrane fixed to the chassis such that the flexible membrane is deformable relative to the chassis; and
an actuation system configured to actuate the reflector, the actuation system including
a support fixed to the chassis,
a plurality of deformation devices, each deformation device of the plurality of deformation devices including a pusher element adapted to be driven in translation relative to the support along a first axis, the pusher element including a part adapted to come into contact with the flexible membrane at a point to deform the flexible membrane,
an actuation device adapted to individually drive the pusher element of each deformation device along the first axis in translation, and
a selector device adapted to move the actuation device toward each deformation device individually, in such a manner that the actuation device is configured to individually drive the pusher element of any deformation device selected from the plurality of deformation devices in translation.
1. An actuation system configured to actuate a reflector including a chassis and a flexible membrane, the flexible membrane being fixed to the chassis such that the flexible membrane is deformable relative to the chassis, the actuation system comprising:
a support fixed to the chassis of the reflector;
a plurality of deformation devices, each deformation device of the plurality of deformation devices including a pusher element adapted to be driven in translation relative to the support along a first axis, the pusher element including a part adapted to come into contact with the flexible membrane at a point to deform the flexible membrane;
an actuation device adapted to individually drive the pusher element of each deformation device along the first axis in translation; and
a selector device adapted to move the actuation device toward each deformation device individually, in such a manner that the actuation device is configured to individually drive the pusher element of any deformation device selected from the plurality of deformation devices in translation.
2. The actuation system according to
3. The actuation system according to
a first rotary element adapted to be driven in rotation relative to the support about a second axis substantially parallel to the first axis by the actuation device, and
a second rotary element connected to an element of the nut/screw system to rotate the element of the nut/screw system with the second rotary element about the first axis and adapted to be driven in rotation about the first axis by the first rotary element.
4. The actuation system according to
5. The actuation system according to
the first rotary elements are distributed over a perimeter of a circle,
the selector device includes a support arm configured to be driven in rotation about a third axis passing through a center of the circle and orthogonal to a plane of the circle, and
the actuation device is fixed to the support arm in such a manner as to be able to individually drive any of the first rotary elements of the deformation devices in rotation.
6. The actuation system according to
7. The actuation system according to
8. The actuation system according to
|
This application claims priority to foreign French patent application No. FR 1100887, filed on Mar. 24, 2011, the disclosure of which is incorporated by reference in its entirety.
The invention lies in the field of antenna reflectors with a deformable reflecting surface. It concerns an actuation system with which such a reflector may be equipped.
A telecommunication satellite includes at least one antenna enabling transmission and reception of electromagnetic signals. Each antenna includes a reflector the shape and the orientation of which determine the terrestrial zone covered by the antenna. With the aim of covering a plurality of distinct terrestrial areas or a terrestrial area more extensive than may be covered with only one antenna, a satellite may include a plurality of antennas, each antenna covering a specific terrestrial zone. However, the number of antennas with which a satellite may be equipped is limited by the space available under the nose cone of the satellite launch vehicle. Moreover, it may be desirable to be able to modify the terrestrial zone covered by an antenna. One solution addressing this two-fold problem is to design an antenna reflector the reflecting surface of which is deformable.
There are known antenna reflectors with a deformable reflecting surface including a flexible membrane and an actuation system comprising a plurality of pusher elements. The flexible membrane may be treated in order to form a reflecting surface. Each pusher element comprises a rod and an actuator of the stepper motor or piezoelectric motor type. Each rod comes into contact with a point on the flexible membrane and may be driven in translation by the actuator in such a manner as to deform the flexible membrane locally. The set of pusher members enables a particular overall shape to be imparted to the flexible membrane. The deformation of the flexible membrane being effected in a discrete manner, it is desirable to increase the number of pusher elements to enable a reflecting surface as smooth and a regular as possible to be formed. However, increasing the number of pusher elements implies an actuation system of high mass, large overall size and high cost. Moreover, each actuator must be supplied with electrical energy and controlled individually. This results in a complex electrical interface. If the actuators are piezoelectric motors, they must be supplied with energy continuously even when they do not have to actuate the rod.
A notable object of the invention is to alleviate some or all of the drawbacks referred to above by proposing an actuation system for an antenna reflector with a deformable reflecting surface that is simple, economic, and light in weight and which enables deformation of the reflecting surface at numerous points. To this end, the invention provides an actuation system with which a reflector may be equipped including a chassis and a flexible membrane fixed to the chassis in such a manner as to be able to be deformed. The actuation system of the invention includes:
In one particular embodiment, the actuation device is adapted to generate a movement of rotation relative to the support about the axis, said movement of rotation transmitting a movement of translation to the pusher element by means of a screw/nut system.
Each deformation device may then further include:
Each first rotary element may include a first pulley and each second rotary element may include a second pulley. Each deformation device then further includes a belt connecting the first pulley to the second pulley. This pulley/belt system enables the deformation devices to be disposed relatively far apart.
Still in one particular embodiment, the first rotary elements are distributed over the perimeter of a circle, the selector device including a support arm that may be driven in rotation about a third axis passing through the centre of the circle and orthogonal to the plane of the circle, the actuation device being fixed to the support arm in such a manner as to be able to drive the first rotary elements of the deformation devices in rotation.
For example, the actuation device includes a motor adapted to drive each first rotary element in rotation about its second axis.
In one particular embodiment, for at least one deformation device, the actuation system further includes an elastic member one of the ends of which is connected to the part of the pusher element adapted to come into contact with the flexible membrane to move with it in translation along the first axis and another end of which is connected to the flexible membrane to move with it in translation along the first axis, the elastic element being elastically deformable along the first axis.
In this particular embodiment the actuation system may include, for each deformation device including an elastic element, a second elastic element one end of which is connected to the support to move with it in translation along the first axis and another end of which is connected to the flexible membrane to move with it in translation along the first axis, the second elastic element being elastically deformable along the first axis, the stiffness of the first elastic element along the first axis being less than the stiffness of the second elastic element along the first axis.
The invention also provides a reflector including a chassis, a flexible membrane fixed to the chassis in such a manner as to be able to be deformed, and an actuation system as described above.
The invention has the notable advantage that it enables the actuation system to include only one actuator for all the deformation points of the flexible membrane.
The invention will be better understood and other advantages will become apparent on reading the following description, which is given with reference to the appended drawings, in which:
The actuation system 23 includes a fixed structure 231 forming a support, a selector device 232, an actuator device 233 and a set of deformation devices 234. In
The actuation device 233 enables the first pulley 2341 of each deformation device 234 and, via the belts 2343, the second pulleys 2342 to be driven in rotation. It includes an actuator 2331, such as a stepper motor or a piezoelectric motor, and a drive part 2332 that may be driven in rotation by the actuator 2331 about an axis substantially parallel to the axis X1. The drive part 2332 is configured so as to be able to be coupled to each first pulley 2341. For example, the drive part 2332 includes a flat screwdriver type tip and the first pulleys 2341 each include an imprint adapted to receive that tip. This type of tip enables engagement and disengagement of the drive part 2332 and the imprint of the first pulley 2341 on movement in rotation of the actuation device 233 by the selector device 232 without necessitating movement in translation along the axis X1. The drive part 2332 must then effect an integer number of half-turn.
The selector device 232 enables movement of the actuation device 233 toward each of the deformation devices 234 in such a manner that the actuation device 233 may drive the first pulley 2341 of the selected deformation device 234 in rotation. In one particular embodiment, the selector device 232 includes an electric motor 2321 and a support arm 2322. The electric motor 2321 is adapted to drive rotation of the support arm 2322 about a third axis X3 substantially parallel to the axes X1 and X2. The actuation device 233 is fixed to the support arm 2322. In this particular embodiment, the first pulleys 2341 of each deformation device 234 are mounted on the fixed structure 231 in a circular arrangement. The actuation device 233 may thus be brought face to face with each pulley 2341 by rotation of the support arm 2322 about the axis X3 and the deformation devices 234 may be actuated successively. Although the placing of the pulleys 2341 is constrained by the circular movement of the actuation device 233, the second pulleys 2342 may be distributed freely over the fixed structure 231 thanks to the belts 2343.
The actuation system 23 has been described with reference to
The mechanical connections between the ends of the threaded rods 2345 and the flexible membrane 12 may, as in the embodiments shown in
Baudasse, Yannick, Vezain, Stéphane
Patent | Priority | Assignee | Title |
9774093, | Mar 20 2015 | The Boeing Company | Automated reflector tuning systems and methdos |
Patent | Priority | Assignee | Title |
5091733, | Apr 18 1989 | Agence Spatiale Europeenne | Antenna pointing device |
5440320, | Jun 19 1991 | Societe Nationale Industrielle et Aerospatiale | Antenna reflector reconfigurable in service |
5831780, | Jan 31 1996 | B F GOODRICH COMPANY, THE | Continually supported thin mirror with force-type actuators |
5976287, | Jun 23 1992 | Commonwealth Scientific and Industrial Research Organisation | Method and apparatus of stud array upstand setting |
20030234970, | |||
20080156938, | |||
20110019295, | |||
FR2678111, | |||
WO2009092901, |
Executed on | Assignor | Assignee | Conveyance | Frame | Reel | Doc |
Mar 23 2012 | Thales | (assignment on the face of the patent) | / | |||
Jun 25 2012 | BAUDASSE, YANNICK | Thales | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 028448 | /0033 | |
Jun 25 2012 | VEZAIN, STEPHANE | Thales | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 028448 | /0033 |
Date | Maintenance Fee Events |
Jan 30 2018 | M1551: Payment of Maintenance Fee, 4th Year, Large Entity. |
Jan 26 2022 | M1552: Payment of Maintenance Fee, 8th Year, Large Entity. |
Date | Maintenance Schedule |
Aug 12 2017 | 4 years fee payment window open |
Feb 12 2018 | 6 months grace period start (w surcharge) |
Aug 12 2018 | patent expiry (for year 4) |
Aug 12 2020 | 2 years to revive unintentionally abandoned end. (for year 4) |
Aug 12 2021 | 8 years fee payment window open |
Feb 12 2022 | 6 months grace period start (w surcharge) |
Aug 12 2022 | patent expiry (for year 8) |
Aug 12 2024 | 2 years to revive unintentionally abandoned end. (for year 8) |
Aug 12 2025 | 12 years fee payment window open |
Feb 12 2026 | 6 months grace period start (w surcharge) |
Aug 12 2026 | patent expiry (for year 12) |
Aug 12 2028 | 2 years to revive unintentionally abandoned end. (for year 12) |